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Understanding
9/11
This image is part of a series that was created for an open textbook, Aerodynamics and Aircraft Performance. The textbook is available here.
Kindred Grey (2021). "Comparison of Constant Power and Constant Thrust Available Cases." CC BY 4.0. Adapted from James F. Marchman (2004). CC BY 4.0.
Alternative text:
The same axes as the previous figure are used, but now with an upward opening parabola labeled Power Required. This parabola intersects with a line of constant slope labeled constant thrust available. A horizontal line is also at a value of cap P times root sigma, labeled constant power available. The minimum of the power required parabola is denoted at h dot sub max for constant cap P, while the intersection between the constant thrust and power available lines is denoted as h dot sub max for constant thrust.
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